Directional control of rockets using elastic deformation of stru

Details Directional control of rockets using elastic deformation of stru Directional control of rockets using elastic deformation of stru

1984-07-26

1987-03-10

Tudor, Harold J.

Aeronautics and astronautics

Missile stabilization or trajectory control

Externally mounted stabilizing appendage

244 321, F42B 1502

Patent

active

046485678

ABSTRACT:
A missile is disclosed which utilizes elastic deformation of structural members in order to control missile flight. The elastic deformation may be in the mounting of the rocket nozzle, the provision of deformable control surfaces, or provision of deformable sections of rocket body, all of which are controlled by independent actuating means.

REFERENCES:
patent: 1166879 (1916-01-01), Alard
patent: 2020759 (1935-11-01), Atwood
patent: 2952207 (1960-09-01), Kamimoto
patent: 3125313 (1964-03-01), Soderberg

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